• 제목/요약/키워드: Thermo-Mechanical Model

검색결과 301건 처리시간 0.029초

돌발화염으로 인한 화상예측에 관한 수치해석적 연구 (Numerical Study on Skin Burn Injury due to Flash Flame Exposure)

  • 이준경;방창훈
    • 한국화재소방학회논문지
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    • 제26권5호
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    • pp.13-20
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    • 2012
  • 매년 많은 소방공무원들이 화재나 고온 조건 등에 노출되어 화상으로 고통 받고 있어, 화상 예측에 대한 연구를 통해 화상을 방지할 수 있는 방법의 개발이 매우 중요하다. 그러나 피부조직의 비선형성, 혈류에 의한 열전달 분석의 불확실성 등 인체 내부의 복잡한 물리현상으로 인해 화상에 대한 연구는 매우 부족한 것이 실정이며, 특히 국내의 경우는 이에 대한 연구가 전무한 실정이다. 본 연구에서는 특히 심각한 화상을 유발할 수 있는 돌발화염(80 kW/$m^2$ 이상의 고열 유속 조건)하에서의 2도 화상 발생에 대한 예측을 수행하였다. 생체 열전달 방정식(Bio-heat transfer)을 이용하여 지배방정식을 유도하였으며, 유한차분법(Finite Difference Method)을 활용하여 화상에 대한 예측을 수행하는 수치해석 접근법을 사용하였다. 기존의 여러 연구결과로부터 인체 피부의 열물성치를 정리하였고, 그것을 바탕으로 계산을 수행하였다. 기존의 낮은 열유속에 대한 화상 실험 결과와 예측 결과를 비교하여 가장 오차가 적은 열물성치 모델을 파악하였고, 그 결과를 바탕으로 고열유속의 돌발화염에서의 2도 화상발생 노출시간을 예측하여 제시하였다.

1500 A, 400 mH급 초전도 직류 리액터용 극저온 냉각 시스템 구조 설계 및 열 해석 (Structure Design and Thermal Analysis of Cryogenic Cooling System for a 1500 A, 400 mH Class HTS DC Reactor)

  • 권다어반;레덧탕;성해진;박민원;유인근
    • 한국산업정보학회논문지
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    • 제23권1호
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    • pp.31-41
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    • 2018
  • 이 논문에서는 대 전류, 고온 초전도 직류 리액터를 위한 전도 냉각 시스템의 구조 설계에 대해 논의하고자 한다. 초전도 자석, 보 빈, 전류 리드, 고정용 구조물 그리고 열 교환기가 포함된 전도 냉각 시스템 부품의 크기를 3D CAD 프로그램을 사용하여 계산하였다. 또한, 최적의 설계 변수를 결정하고 열적-기계적 특성을 분석하기 위해서 유한 요소법 모델을 제작하였다. 리액터 자석의 운전 전류와 인덕턴스는 각각 1,500 A 400 mH이며, 이에 따른 극저온 냉동기의 냉각 용량을 결정하기 위해 초전도 직류 리액터에서 발생하는 열 부하를 계산하였다. 또한, 대 전류가 흐르는 1 단부전도 냉각 시스템의 작동 테스트를 수행하였다. 구리 바는 40 K까지 냉각되었고 초전도 리드는 안정적으로 작동했다. 실험 결과로써, 1 단부 영역의 총 열 부하는 190 W였다. 본 연구 결과는 상용 초전도 직류 리액터의 설계 및 제조에 있어 효과적으로 활용 될 것이다.

Modelling of aluminium foam sandwich panels

  • D'Alessandro, Vincenzo;Petrone, Giuseppe;De Rosa, Sergio;Franco, Francesco
    • Smart Structures and Systems
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    • 제13권4호
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    • pp.615-636
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    • 2014
  • Aluminium Foam Sandwich (AFS) panels are becoming always more attractive in transportation applications thanks to the excellent combination of mechanical properties, high strength and stiffness, with functional ones, thermo-acoustic isolation and vibration damping. These properties strongly depend on the density of the foam, the morphology of the pores, the type (open or closed cells) and the size of the gas bubbles enclosed in the solid material. In this paper, the vibrational performances of two classes of sandwich panels with an Alulight(R) foam core are studied. Experimental tests, in terms of frequency response function and modal analysis, are performed in order to investigate the effect of different percentage of porosity in the foam, as well as the effect of the random distribution of the gas bubbles. Experimental results are used as a reference for developing numerical models using finite element approach. Firstly, a sensitivity analysis is performed in order to obtain a limit-but-bounded dynamic response, modelling the foam core as a homogeneous one. The experimental-numerical correlation is evaluated in terms of natural frequencies and mode shapes. Afterwards, an update of the previous numerical model is presented, in which the core is not longer modelled as homogeneous. Mass and stiffness are randomly distributed in the core volume, exploring the space of the eigenvectors.

The Review of Studies on Pressure Drop and Heat Transfer In Microchannels

  • Hwang, Yun-Wook;Kim, Min-Soo
    • International Journal of Air-Conditioning and Refrigeration
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    • 제13권1호
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    • pp.51-60
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    • 2005
  • This paper reviews the studies on the pressure drop and the heat transfer in microchannels. Although a lot of studies about the single-phase flow have been done until now, conflicting results are occasionally reported about flow transition from laminar flow to turbulent flow, friction factor, and Nusselt number. Some studies reported the early flow transition due to relatively greater wall effect like surface roughness, but the other studies showed that the flow transition occurred at the Reynolds number of about 2300 and the early flow transition might be due to less accurate measurement of the channel geometry. Also, there have been arguments whether the conventional relation based upon continuum theory can be applied to the fluid flow and the heat transfer in microchannels without modification or not. The studies about the two-phase flow in microchannels have been mostly about investigating the flow pattern and the pressure drop in rectangular channels using two-component, two-phase flow like air/water mixture. Some studies proposed correlations to predict two-phase flow pressure drop in microchannels. They were mostly based on Lockhart-Martinelli model with modification on C-coefficient, which was dependent on channel geometry, Reynolds number, surface tension, and so on. Others investigated the characteristics of flow boiling heat transfer in microchannels with respect to test parameters such as mass flux, heat flux, system pressure, and so on. The existing studies have not been fully satisfactory in providing consistent results about the pressure drop and the heat transfer in microchannels. Therefore, more in-depth studies should be done for understanding the fundamentals of the transport phenomena in the microchannels and giving the basic guidelines to design the micro devices.

Reliable Anisotropic Conductive Adhesives Flip Chip on Organic Substrates For High Frequency Applications

  • Paik, Kyung-Wook;Yim, Myung-Jin;Kwon, Woon-Seong
    • 한국마이크로전자및패키징학회:학술대회논문집
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    • 한국마이크로전자및패키징학회 2001년도 Proceedings of 6th International Joint Symposium on Microeletronics and Packaging
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    • pp.35-43
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    • 2001
  • Flip chip assembly on organic substrates using ACAs have received much attentions due to many advantages such as easier processing, good electrical performance, lower cost, and low temperature processing compatible with organic substrates. ACAs are generally composed of epoxy polymer resin and small amount of conductive fillers (less than 10 wt.%). As a result, ACAs have almost the same CTE values as an epoxy material itself which are higher than conventional underfill materials which contains lots of fillers. Therefore, it is necessary to lower the CTE value of ACAs to obtain more reliable flip chip assembly on organic substrates using ACAs. To modify the ACA composite materials with some amount of conductive fillers, non-conductive fillers were incorporated into ACAs. In this paper, we investigated the effect of fillers on the thermo-mechanical properties of modified ACA composite materials and the reliability of flip chip assembly on organic substrates using modified ACA composite materials. Contact resistance changes were measured during reliability tests such as thermal cycling, high humidity and temperature, and high temperature at dry condition. It was observed that reliability results were significantly affected by CTEs of ACA materials especially at the thermal cycling test. Results showed that flip chip assembly using modified ACA composites with lower CTEs and higher modulus by loading non-conducting fillers exhibited better contact resistance behavior than conventional ACAs without non-conducting fillers. Microwave model and high-frequency measurement of the ACF flip-chip interconnection was investigated using a microwave network analysis. ACF flip chip interconnection has only below 0.1nH, and very stable up to 13 GHz. Over the 13 GHz, there was significant loss because of epoxy capacitance of ACF. However, the addition of $SiO_2filler$ to the ACF lowered the dielectric constant of the ACF materials resulting in an increase of resonance frequency up to 15 GHz. Our results indicate that the electrical performance of ACF combined with electroless Wi/Au bump interconnection is comparable to that of solder joint.

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기능경사 소재 등가 물성치 예측을 위한 균질화 기법의 특성분석을 위한 수치해석 (Numerical Analysis for the Characteristic Investigation of Homogenization Techniques Used for Equivalent Material Properties of Functionally Graded Material)

  • 조진래;최주형;신대섭
    • 한국전산구조공학회논문집
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    • 제21권1호
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    • pp.13-20
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    • 2008
  • 기능경사 소재(FGM)에는 서로 다른 두 가지 구성입자들이 혼합되어 있는 경사층(graded layer)이 삽입되어, 소재 전 영역에 걸쳐 구성입자의 체적분율이 연속적이고 기능적으로 변화하도록 되어있다. 이러한 이상(dual-phase) 입자복합재의 열 기계적 거동을 해석함에 있어 필수적인 경사층의 물성치는 전통적으로 균질화 기법을 이용하여 예측되었다. 하지만, 이러한 균질화 기법은 구성입자의 형태, 분산구조 등과 같은 상세 형상을 반영하지 못하지 때문에 복합재의 총체적인 등가 물성치 예측에만 국한 되어왔다. 이러한 맥락에서 본 연구에서는 경사층을 미시역학적으로 이산화 모델링하고, 다양한 체적분율과 외부 하중조건에 대해 유한요소해석을 실시하여 이러한 균질화 기법들의 특성을 분석하였다.

인공신경망을 이용한 선상가열 공정의 역학정보모델 (A Mechanical Information Model of Line Heating Process using Artificial Neural Network)

  • 박성건;김원돈;신종계
    • 대한조선학회논문집
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    • 제34권1호
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    • pp.122-129
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    • 1997
  • 외판곡가공 과정의 역학적해석에 사용되는 열탄소성 해석은 계산시간이 많이 소요된다. 선상가열작업의 최적공정을 구하기 위하여는 시뮬레이션과 유한요소해석 사이에 상당수의 반복계산이 필요하다. 그러므로 요구되는 천문학적인 계산시간으로 인하여 선상가열의 수치시뮬레이션은 많은 제약을 받고 있다. 따라서 선상가열의 시뮬레이션에 소요되는 역학해석 계산시간을 크게 줄이는 방안이 필요하다. 외판곡가공에서의 역학적 정보를 효율적으로 구하기 위하여, 본 논문에서는 먼저 선상 가열 작업에 영향을 끼치는 요소들을 살펴보았으며, 역전파 방식의 인공 신경망을 이용하여 일종의 추론기구를 구현하였다. 신경망은 은닉층의 갯수와 은닉층에 있는 뉴런의 갯수를 바꿔 주며 수치해석 결과들을 학습시켰다. 그 결과 두개의 은닉층을 가진 인공 신경망의 경우 각 은닉층에 뉴런의 갯수가 충분하다면 학습 예제들을 쉽게 학습하였고, 또 학습된 결과로부터 새로운 해를 도출해 낼 때 그 값은 실제 값과 비교해 볼 때 비교적 작은 오차를 보였다. 결과적으로 구하고자 하는 문제영역 근처에 충분한 학습 예제가 마련된다면 비교적 실제 값에 근사하는 결과를 보인다는 것을 알 수 있었다. 본 연구를 통하여, 수치해석결과의 학습방법을 기초로한 인공신경망은 곡면가공의 시뮬레이션단계에서 필요한 역학적 해석정보의 경제적인 산출에 적용가능함이 확인되었다.

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융해-동결작용을 고려한 말뚝 기초에 관한 수치해석 연구 (Numerical Analysis of Pile Foundation Considering the Thawing and Freezing Effects)

  • 박우진;박동수;신문범;서영교
    • 한국지반공학회논문집
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    • 제39권5호
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    • pp.51-63
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    • 2023
  • 계절성 동토의 온도 변화에 따른 융해 및 동결작용에 의한 지반의 거동이 말뚝 기초의 변위 및 지지력에 끼치는 영향을 파악하기 위한 수치해석을 수행하였다. 수치해석은 온도 변화에 따른 지반-말뚝 상호작용을 모사하기 위해 유한요소법 기반의 TM 모델링(Thermo-Mechanical coupled Modeling)을 적용하였으며, 동결 지반은 온도 의존적 비선형 물성을 적용하였다. 지반의 구성 모델은 소성 거동을 모사하기 위한 MCR 모델(Mohr Coulomb with Rankine Tensile cut-off Model)과 HDP 모델(Nonlinear Hyperbolic Drucker-Prager Model)을 각각 적용하였으며, 말뚝의 길이 및 너비 조건을 선정해 수치해석 결과를 비교 및 분석하였다. 수치해석 결과는 HDP 구성 모델이 비교적 작은 지반 거동과 지지력을 보였으나, 전체적으로는 말뚝의 길이 및 너비 조건에 따라 지지력 및 말뚝 머리의 변위 결과의 양상과 그 크기는 유사하게 나타났다. 지반의 융해-동결작용으로 인한 말뚝 머리(pile head)의 수직 변위는 길이 조건이 짧을수록 변위의 변화 폭이 크게 나타났다. 수직 변위는 길이 조건에 따라 MCR 구성 모델에서는 최대 0.0387m의 융해 침하와 0.0277m의 동결 융기가 발생했으며, HDP 구성 모델에서는 최대 0.0367m의 융해 침하와 0.0264m의 동결 융기가 발생했다. 또한 두 탄소성 모델에 대한 말뚝의 지지력 결과는 말뚝의 길이 조건보다 너비 조건에서 더 큰 차이를 보였으며, 너비 조건 L에서 최대 약 14.7%, M에서 최대 약 5.4%, S에서 최대 약 5.3%가 발생하였다. 이에 말뚝 머리의 수직 변위와 말뚝의 지지력은 말뚝-지반의 접촉 면적에 영향을 크게 받으며, 지반 내 활성층의 활성도에 따라 차이를 보였다.

AI-Li계 합금의 초소성에 관한 연구 (Study on the Superplasticity in Al-Li Alloy Systems)

  • 진영철;국진선;김양수;홍은성;이민상;이민호;유창영
    • 열처리공학회지
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    • 제5권1호
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    • pp.41-49
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    • 1992
  • The effects of alloying elements on the superplastic properties of Al-Li based alloys had been investigated. The intermediate thermo-mechanical treated (ITMT) Al-2.0wt%Li, Al-2.0wt%Li-1.0wt%Mg, Al-2.0wt%Li-0.12wt%Zr and Al-2.0wt%Li-1.2wt%Cu-1.0wt%Mg-0.12wt%Zr alloys were tested in tension at various temperature (400, 450, 500 and $550^{\circ}C$) and strain rate($6.7{\times}10^{-3}$, $1.0{\times}10^{-2}$, $1.6{\times}10^{-2}$ and $5.0{\times}10^{-2}/sec$). The results were as follows : The superplasticity in binary, ternary and pentanary alloys appeared at 500 to $550^{\circ}C$, and good strain rate for superplasticity. $1.6{\times}10^{-2}/sec{\sim}1.0{\times}10^{-2}/sec$ for a binary alloy and $1.0{\times}10^{-2}/sec{\sim}6.7{\times}10^{-3}/sec$ for ternary and pentanary alloys. A Zr-added ternary alloy had best value of elongation (730%) in four alloys at $550^{\circ}C$ of tension temperature and $1.0{\times}10^{-2}/sec$ of strain rate. The strain rate was greatly dependent on tension temperature and true strain rate was more than 1.0 at all test temperature and strain rate. In binary and Mg-added teranry alloys. the necks were slightly formed and their fracture surface had lips shape, but Zr-added ternary and pentanary alloy fractured along the grain boundary without necking. Their dislocations moved to grain boundary during superplasticity deformation and arranged perpendicular to grain boundary. Super plastic deformation was made by grain boundary slip of dislocation slip creep and model of core and mantle.

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Recent research activities on hybrid rocket in Japan

  • Harunori, Nagata
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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    • pp.1-2
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    • 2011
  • Hybrid rockets have lately attracted attention as a strong candidate of small, low cost, safe and reliable launch vehicles. A significant topic is that the first commercially sponsored space ship, SpaceShipOne vehicle chose a hybrid rocket. The main factors for the choice were safety of operation, system cost, quick turnaround, and thrust termination. In Japan, five universities including Hokkaido University and three private companies organized "Hybrid Rocket Research Group" from 1998 to 2002. Their main purpose was to downsize the cost and scale of rocket experiments. In 2002, UNISEC (University Space Engineering Consortium) and HASTIC (Hokkaido Aerospace Science and Technology Incubation Center) took over the educational and R&D rocket activities respectively and the research group dissolved. In 2008, JAXA/ISAS and eleven universities formed "Hybrid Rocket Research Working Group" as a subcommittee of the Steering Committee for Space Engineering in ISAS. Their goal is to demonstrate technical feasibility of lowcost and high frequency launches of nano/micro satellites into sun-synchronous orbits. Hybrid rockets use a combination of solid and liquid propellants. Usually the fuel is in a solid phase. A serious problem of hybrid rockets is the low regression rate of the solid fuel. In single port hybrids the low regression rate below 1 mm/s causes large L/D exceeding a hundred and small fuel loading ratio falling below 0.3. Multi-port hybrids are a typical solution to solve this problem. However, this solution is not the mainstream in Japan. Another approach is to use high regression rate fuels. For example, a fuel regression rate of 4 mm/s decreases L/D to around 10 and increases the loading ratio to around 0.75. Liquefying fuels such as paraffins are strong candidates for high regression fuels and subject of active research in Japan too. Nakagawa et al. in Tokai University employed EVA (Ethylene Vinyl Acetate) to modify viscosity of paraffin based fuels and investigated the effect of viscosity on regression rates. Wada et al. in Akita University employed LTP (Low melting ThermoPlastic) as another candidate of liquefying fuels and demonstrated high regression rates comparable to paraffin fuels. Hori et al. in JAXA/ISAS employed glycidylazide-poly(ethylene glycol) (GAP-PEG) copolymers as high regression rate fuels and modified the combustion characteristics by changing the PEG mixing ratio. Regression rate improvement by changing internal ballistics is another stream of research. The author proposed a new fuel configuration named "CAMUI" in 1998. CAMUI comes from an abbreviation of "cascaded multistage impinging-jet" meaning the distinctive flow field. A CAMUI type fuel grain consists of several cylindrical fuel blocks with two ports in axial direction. The port alignment shifts 90 degrees with each other to make jets out of ports impinge on the upstream end face of the downstream fuel block, resulting in intense heat transfer to the fuel. Yuasa et al. in Tokyo Metropolitan University employed swirling injection method and improved regression rates more than three times higher. However, regression rate distribution along the axis is not uniform due to the decay of the swirl strength. Aso et al. in Kyushu University employed multi-swirl injection to solve this problem. Combinations of swirling injection and paraffin based fuel have been tried and some results show very high regression rates exceeding ten times of conventional one. High fuel regression rates by new fuel, new internal ballistics, or combination of them require faster fuel-oxidizer mixing to maintain combustion efficiency. Nakagawa et al. succeeded to improve combustion efficiency of a paraffin-based fuel from 77% to 96% by a baffle plate. Another effective approach some researchers are trying is to use an aft-chamber to increase residence time. Better understanding of the new flow fields is necessary to reveal basic mechanisms of regression enhancement. Yuasa et al. visualized the combustion field in a swirling injection type motor. Nakagawa et al. observed boundary layer combustion of wax-based fuels. To understand detailed flow structures in swirling flow type hybrids, Sawada et al. (Tohoku Univ.), Teramoto et al. (Univ. of Tokyo), Shimada et al. (ISAS), and Tsuboi et al. (Kyushu Inst. Tech.) are trying to simulate the flow field numerically. Main challenges are turbulent reaction, stiffness due to low Mach number flow, fuel regression model, and other non-steady phenomena. Oshima et al. in Hokkaido University simulated CAMUI type flow fields and discussed correspondence relation between regression distribution of a burning surface and the vortex structure over the surface.

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